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altitude.
2. The n = 1.3 g (n = 1.4 g) curve indicates the buffet margin.
OPTIMUM WEIGHT FOR FEET STEP CLIMB
WEIGHT (1 000 kg/1 000 lb)
STEP CLIMB FROM/TO ≤ ISA +10 ISA +15 ISA +20
LR M .78 LR M .78 LR M .78
310/350 75/165 75/165 74/163 73/160 72/158 69/152
330/370 68/149 68/149 68/149 67/147 66/145 64/141
350/390 61/134 62/136 61/134 61/134 60/132 58/127
BLEED CORRECTIONS
ENGINE ANTI ICE TOTAL ANTI ICE
ISA OMpatx AAltlt.. :: -N 9o0 c0o frtr. OMpatx AAltlt.. :: -N1o 5 c0o0r rf.t
ISA +10 OMpatx AAltlt.. :: -N 9o0 c0o frtr. OMpatx AAltlt.. :: -N1o 6 c0o0r rf.t
ISA +15 OMpatx AAltlt.. :: -N 9o0 c0o frtr. OMpatx .A Alt.lt. :: -N1o 7 c0o0r rf.t
To be continued on next page
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
CRUISE
ALL ENGINES OPERATIVE - ALTITUDE
A318/A319/A320/A321 FLEET PER-CRZ-AEO-ALT-10 P 2/16
FCOM 19 AUG 10
Continued from previous page
ENGINE ANTI ICE TOTAL ANTI ICE
ISA +20 OMpatx AAltlt.. :: --1100 fftt OMpatx AAltlt.. :: --2200 fftt
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
CRUISE
ALL ENGINES OPERATIVE - ALTITUDE
A318/A319/A320/A321 FLEET PER-CRZ-AEO-ALT-10 P 3/16
FCOM 19 AUG 10
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
CRUISE
ALL ENGINES OPERATIVE - ALTITUDE
A318/A319/A320/A321 FLEET PER-CRZ-AEO-ALT-10 P 4/16
FCOM 19 AUG 10
CRUISE LEVEL CHARTS
Applicable to: MSN,
These charts have been established for a center of gravity at 33 % MAC.
Maximum and optimum altitudes are given for different temperatures at long range speed and M .78.
Note: 1. Optimum and maximum altitudes curves do not cover for M .78 the whole weight range
because above a given weight these Mach numbers cannot be maintained, whatever the
altitude.
2. The n = 1.3 g (n = 1.4 g) curve indicates the buffet margin.
OPTIMUM WEIGHT FOR FEET STEP CLIMB
WEIGHT (1 000 kg/1 000 lb)
STEP CLIMB FROM/TO ≤ ISA +10 ISA +15 ISA +20
LR M .78 LR M .78 LR M .78
310/350 82/180 82/180 80/176 80/176 77/169 76/167
330/370 74/163 75/165 73/160 73/160 69/152 69/152
350/390 67/147 68/149 66/145 66/145 63/138 63/138
BLEED CORRECTIONS
ENGINE ANTI ICE TOTAL ANTI ICE
≤ ISA +10 OMpatx AAltlt.. :: --00 fftt OMpatx AAltlt.. :: -- 13 0f tft
ISA +15 OMpatx AAltlt.. :: --00 fftt OMpatx .A Alt.lt. :: -- 16 0f tft
ISA +20 OMpatx AAltlt.. :: --1100 fftt OMpatx AAltlt.. :: --2200 fftt
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
CRUISE
ALL ENGINES OPERATIVE - ALTITUDE
A318/A319/A320/A321 FLEET PER-CRZ-AEO-ALT-10 P 5/16
FCOM 19 AUG 10
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
CRUISE
ALL ENGINES OPERATIVE - ALTITUDE
A318/A319/A320/A321 FLEET PER-CRZ-AEO-ALT-10 P 6/16
FCOM 19 AUG 10
CRUISE LEVEL CHARTS
Applicable to: MSN,
These charts have been established for a center of gravity at 33 % MAC.
Maximum and optimum altitudes are given for different temperatures at long range speed and M .78.
Note: 1. Optimum and maximum altitudes curves do not cover for M .78 the whole weight range
because above a given weight these Mach numbers cannot be maintained, whatever the
altitude.
2. The n = 1.3 g (n = 1.4 g) curve indicates the buffet margin.
OPTIMUM WEIGHT FOR FEET STEP CLIMB
WEIGHT (1 000 kg/1 000 lb)
STEP CLIMB FROM/TO ≤ ISA +10 ISA +15 ISA +20
LR M .78 LR M .78 LR M .78
310/350 75/165 75/165 74/163 73/160 70/154 69/152
330/370 68/149 69/152 68/149 67/147 64/141 64/141
350/390 61/134 62/136 61/134 61/134 58/127 57/125
BLEED CORRECTIONS
ENGINE ANTI ICE TOTAL ANTI ICE
≤ ISA + 10 OMpatx AAltlt.. :: -N 9o0 c0o frtr. OMpatx AAltlt.. :: -N1o 7 c0o0r rf.t
ISA +15 OMpatx AAltlt.. :: -N1o 4 c0o0r rf.t OMpatx AAltlt.. :: --1200 fftt
ISA +20 OMpatx AAltlt.. :: --1100 fftt OMpatx .A Alt.lt. :: --2200 fftt
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
CRUISE
ALL ENGINES OPERATIVE - ALTITUDE
A318/A319/A320/A321 FLEET PER-CRZ-AEO-ALT-10 P 7/16
FCOM 19 AUG 10
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
CRUISE
ALL ENGINES OPERATIVE - ALTITUDE
A318/A319/A320/A321 FLEET PER-CRZ-AEO-ALT-10 P 8/16
FCOM 19 AUG 10
CRUISE LEVEL CHARTS
Applicable to:
These charts have been established for a center of gravity at 33 % MAC.
Maximum and optimum altitudes are given for different temperatures at long range speed and M .78.
Note: 1. Optimum and maximum altitudes curves do not cover for M .78 the whole weight range
because above a given weight these Mach numbers cannot be maintained, whatever the
　
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